ATE556195T1 - Ringförmige schaufelanordnung für einen gasturbinenmotor - Google Patents

Ringförmige schaufelanordnung für einen gasturbinenmotor

Info

Publication number
ATE556195T1
ATE556195T1 AT09152225T AT09152225T ATE556195T1 AT E556195 T1 ATE556195 T1 AT E556195T1 AT 09152225 T AT09152225 T AT 09152225T AT 09152225 T AT09152225 T AT 09152225T AT E556195 T1 ATE556195 T1 AT E556195T1
Authority
AT
Austria
Prior art keywords
rail
assembly
strip
vane
main body
Prior art date
Application number
AT09152225T
Other languages
German (de)
English (en)
Inventor
Philip Twell
Original Assignee
Siemens Ag
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens Ag filed Critical Siemens Ag
Application granted granted Critical
Publication of ATE556195T1 publication Critical patent/ATE556195T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
AT09152225T 2009-02-05 2009-02-05 Ringförmige schaufelanordnung für einen gasturbinenmotor ATE556195T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP09152225A EP2216511B1 (en) 2009-02-05 2009-02-05 An annular vane assembly for a gas turbine engine

Publications (1)

Publication Number Publication Date
ATE556195T1 true ATE556195T1 (de) 2012-05-15

Family

ID=40602561

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09152225T ATE556195T1 (de) 2009-02-05 2009-02-05 Ringförmige schaufelanordnung für einen gasturbinenmotor

Country Status (6)

Country Link
US (1) US8398366B2 (es)
EP (1) EP2216511B1 (es)
CN (1) CN101798940B (es)
AT (1) ATE556195T1 (es)
ES (1) ES2382938T3 (es)
RU (1) RU2511770C2 (es)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100068050A1 (en) * 2008-09-12 2010-03-18 General Electric Company Gas turbine vane attachment
FR2967730B1 (fr) * 2010-11-24 2015-05-15 Snecma Etage de compresseur dans une turbomachine
GB201105788D0 (en) * 2011-04-06 2011-05-18 Rolls Royce Plc Stator vane assembly
US8920116B2 (en) * 2011-10-07 2014-12-30 Siemens Energy, Inc. Wear prevention system for securing compressor airfoils within a turbine engine
US8899914B2 (en) * 2012-01-05 2014-12-02 United Technologies Corporation Stator vane integrated attachment liner and spring damper
US8920112B2 (en) * 2012-01-05 2014-12-30 United Technologies Corporation Stator vane spring damper
US9506361B2 (en) * 2013-03-08 2016-11-29 Pratt & Whitney Canada Corp. Low profile vane retention
US9206700B2 (en) * 2013-10-25 2015-12-08 Siemens Aktiengesellschaft Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine
US10329931B2 (en) 2014-10-01 2019-06-25 United Technologies Corporation Stator assembly for a gas turbine engine
EP3009608B1 (en) * 2014-10-02 2019-10-30 United Technologies Corporation Vane assembly with trapped segmented vane structures
US10107125B2 (en) * 2014-11-18 2018-10-23 United Technologies Corporation Shroud seal and wearliner
US9790809B2 (en) 2015-03-24 2017-10-17 United Technologies Corporation Damper for stator assembly
JP6614407B2 (ja) 2015-06-10 2019-12-04 株式会社Ｉｈｉ タービン
US10330009B2 (en) 2017-01-13 2019-06-25 United Technologies Corporation Lock for threaded in place nosecone or spinner
US10612405B2 (en) * 2017-01-13 2020-04-07 United Technologies Corporation Stator outer platform sealing and retainer
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
CN109209518B (zh) * 2018-10-29 2020-12-22 江苏海事职业技术学院 一种燃气轮机透平静叶定位结构
US11156110B1 (en) 2020-08-04 2021-10-26 General Electric Company Rotor assembly for a turbine section of a gas turbine engine
JP7465374B2 (ja) 2021-02-05 2024-04-10 三菱重工業株式会社 静翼環、及び回転機械
US11655719B2 (en) 2021-04-16 2023-05-23 General Electric Company Airfoil assembly
CN113898421A (zh) * 2021-10-10 2022-01-07 中国航发沈阳发动机研究所 一种压气机静子内环及其转静子封严连接结构
US12071864B2 (en) 2022-01-21 2024-08-27 Rtx Corporation Turbine section with ceramic support rings and ceramic vane arc segments
KR102707857B1 (ko) * 2022-02-07 2024-09-23 두산에너빌리티 주식회사 베인 팁 간극을 최소화할 수 있는 압축기 및 이를 포함하는 가스터빈
KR102707856B1 (ko) 2022-02-07 2024-09-23 두산에너빌리티 주식회사 베인 팁 간극을 최소화할 수 있는 압축기 및 이를 포함하는 가스터빈

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3326523A (en) * 1965-12-06 1967-06-20 Gen Electric Stator vane assembly having composite sectors
FR2282550A1 (fr) * 1974-08-21 1976-03-19 Shur Lok International Sa Stator de compresseur a carter monobloc
IT1062412B (it) * 1976-06-15 1984-10-10 Nuovo Pignone Spa Sistema perfezionato di bloccaggio in posizione delle pale sulla casca statorica di un compressore assiale operante in ambiente pulverulento
SU1071776A1 (ru) * 1982-11-03 1984-02-07 Куйбышевский авиационный институт им.акад.С.П.Королева Статор турбомашины
US4897021A (en) * 1988-06-02 1990-01-30 United Technologies Corporation Stator vane asssembly for an axial flow rotary machine
GB2250782B (en) * 1990-12-11 1994-04-27 Rolls Royce Plc Stator vane assembly
FR2702242B1 (fr) * 1993-03-03 1995-04-07 Snecma Etage d'aubes libres à une extrémité.
US5927942A (en) * 1993-10-27 1999-07-27 United Technologies Corporation Mounting and sealing arrangement for a turbine shroud segment
US7291946B2 (en) * 2003-01-27 2007-11-06 United Technologies Corporation Damper for stator assembly
FR2906296A1 (fr) * 2006-09-26 2008-03-28 Snecma Sa Dispositif de fixation d'une aube fixe dans un carter annulaire de turbomachine, turboreacteur incorporant le dispositif et procede de montage de l'aube.
FR2918108B1 (fr) * 2007-06-26 2009-10-02 Snecma Sa Dispositif amortisseur pour stator de turbomachine

Also Published As

Publication number Publication date
EP2216511B1 (en) 2012-05-02
US8398366B2 (en) 2013-03-19
EP2216511A1 (en) 2010-08-11
ES2382938T3 (es) 2012-06-14
US20100196155A1 (en) 2010-08-05
RU2511770C2 (ru) 2014-04-10
CN101798940B (zh) 2014-08-13
CN101798940A (zh) 2010-08-11
RU2010103841A (ru) 2011-08-10

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